Airworthiness Directive 46-17-01
one-timeAirworthiness Directives; certification or at first periodic inspection thereafter. Inspect the universal joint pins in the flap control push-pull tubes, P/
Which aircraft AD 46-17-01 applies to
Inspect universal joint pins in flap control push-pull tubes (P/N 19-152642) connecting outer and inner flap for broken pins; replace broken pins and install a close-fitting rubber hose over each universal joint; required at certification or first periodic inspection thereafter; specific North American model not stated in excerpt.
Whether AD 46-17-01 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.